Airframe design for modularity of the BWB Baseline II-E2 UAV

This paper discusses the airframe design of UiTM's Blended Wing Body (BWB) Baseline II-E2 Unmanned Aerial Vehicle (UAV). The design concept is based on the modularity. The BWB airframe was modeled by using Computer Aided Design (CAD) software. Static analysis on the BWB airframe was conducted by using the Finite Element (FE) analysis. Airframe design, stress and displacement contours are presented.